This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: ISRO. Used on stages: GSLV-1, PSLV-1. Used on launch vehicles: GSLV, PSLV. Gross Mass: 160,200 kg. Empty Mass: 31,200 kg. Propellants: Solid Thrust(vac): 495,590 kgf. Thrust(vac): 4,860.00 kN. Isp: 264 sec. Isp (sea level): 237 sec. Burn time: 97 sec. Diameter: 2.8 m. Length: 20.3 m. Chambers: 1. Chamber Pressure: 58.00 bar. Area Ratio: 8.00. Country: India. Status: In Production. First Flight: 1993. Last Flight: 1997. Flown: 4.
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Last update 12 March 2001.
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© Mark Wade, 2001 .